Method for axial and rotational retaining a ball bearing cartridge in the housing of a turbomaschine

Description

TECHNICAL FIELD

[0001] Subject matter disclosed herein relates generally to turbomachinery for internal combustion engines and, in particular, rolling element bearing cartridges and bearing housings for such bearing cartridges.

BACKGROUND

[0002] The advantages associated with low friction bearings are well known to a multitude of varied industries. High-speed applications with DN (dynamic number) values over 1,000,000 are common place for turbomachinery. These high-speed applications, owing to the fact that rotor imbalance force increases as a square function of rotor speed, require damping. Without damping, transmitted forces through the system would cause many well-known problems such as noise, fretting, loosening of joints, and overall reduced service life. Further, the bearings themselves would have unacceptable life. For these reasons, turbomachinery bearings are not hard mounted within their housings. The skilled rotordynamics design engineer spends the majority of his/her life managing these forces, especially those forces encountered as the rotor goes through its natural frequencies, commonly referred to as "critical speeds".

[0003] Most turbochargers that employ a low friction rolling element bearing use two angular contact ball bearings, with each accepting the thrust load in a given axial direction, that are joined together in what is commonly referred to as a "cartridge". In a cylindrical coordinate system a bearing may be defined with respect to axial, radial and azimuthal dimensions. Within a bearing housing, referred to as housing in subsequent text, a cartridge is located axially and azimuthally via one or more mechanisms. For proper functioning, some movement can occur in a radial direction along a radial line typically defined by an azimuthal locating mechanism.

[0004] Conventional bearing cartridge and housing assemblies typically rely on an axial thrust load pin to locate the cartridge axially and azimuthally within a housing. Such pins have a limited ability to align the cartridge in a housing and receive most of the thrust load. Consequently, axial thrust load pins can raise serious wear and misalignment issues.

[0005] An example of a conventional bearing cartridge and housing assembly for a turbocharger with means to limit movement of the outer race with respect to the housing is known from document US 4 721 441 A, where the assembly comprises a housing with a substantially cylindrical bore, a counterbore having a smaller inner diameter at one end and a retainer plate having a smaller inner diameter at the other end. The counterbore and retainer plate limit axial movement of the bearing cartridge in the housing. The housing and the cartridge further comprise opposing recesses at their inner respectively outer diameter at their end proximate the retainer plate to receive a pin to prevent rotation of the bearing cartridge in the housing.

[0006] Overall, an industry need exists for rolling element bearings and/or housings that allow for better alignment and/or reduced wear. Various exemplary bearing cartridges and housings presented herein address such issues and optionally other issues.

Summary of Invention

[0007] According to the present invention, there is provided a method of limiting movement of an outer race of a bearing cartridge with respect to a housing comprising: positioning the bearing cartridge in a substantially cylindrical bore having a longitudinal axis, an inner diameter exceeding an outer diameter of the outer race, a proximate end and a distal end; limiting axial movement of the outer race at the distal end of the cylindrical bore with a counterbore substantially coaxial to the cylindrical bore and having an inner diameter less than the outer diameter of the outer race; limiting axial movement of the outer race at the proximate end of the cylindrical bore with a plate positioned substantially orthogonal to the longitudinal axis; and limiting rotation of the outer race with a pin positioned in a pin opening of the housing accessible via a lubricant drain.

Brief Description of the Drawings

[0008] A more complete understanding of the various methods, devices, systems, arrangements, etc., described herein, and equivalents thereof, may be had by reference to the following detailed description when taken in conjunction with accompanying drawings wherein;

Fig. 1A is a perspective view diagram ofa prior art bearing cartridge for a turbocharger.

Fig. 1B is a diagram of a prior art bearing cartridge in a prior art housing.

Fig. 2 is a perspective view diagram of an exemplary bearing cartridge that does not include an aperture to receive an axial thrust load pin.

Fig. 3 is a side view of an exemplary bearing cartridge that does not include an aperture to receive an axial thrust load pin.

Fig. 4 is a cross-sectional view of an exemplary assembly that includes an exemplary housing and an exemplary bearing cartridge.

Fig. 5 is a cross-sectional view of an exemplary housing that includes features for axially locating a bearing cartridge.

Fig. 6 is front view of an exemplary housing assembly that includes a retaining mechanism that acts to axially locate a bearing cartridge in the housing assembly.

Fig. 7 is a cross-sectional side view of an exemplary retaining mechanism that acts to axially locate a bearing cartridge in a housing.

Fig. 8 is a cross-sectional side view of an exemplary bearing cartridge that includes various outer surface regions.

Fig. 9A is a cross-sectional side view of an exemplary housing that includes two regions with different inner diameters to thereby allow for formation of, for example, two film regions in conjunction with a bearing cartridge.

Fig. 9B is a cross-sectional top view of an exemplary housing that includes two regions with different inner diameters to thereby allow for formation of, for example, two film regions in conjunction with a bearing cartridge.

DETAILED DESCRIPTION

[0009] Various exemplary methods, devices, systems, arrangements, etc., disclosed herein address issues related to technology associated with turbochargers and are optionally suitable for use with electrically assisted turbochargers.

[0010] Fig. 1A shows a perspective view of prior art bearing cartridge 100. A cylindrical coordinate system is shown for reference that includes radial (r), axial (x) and azimuthal (Θ) dimensions. The cartridge 100 includes two annular wells 104, 104' positioned on an outer race 105 intermediate a center section 106 and respective ends of the cartridge 100. The center section 106 of the cartridge 100 includes an opening 108 that cooperates with a pin to position the cartridge 100 axially and azimuthally in a housing or journal. For example, conventional bearing cartridges for turbomachinery often rely on an axial thrust load pin that is received by such an opening to axially locate the bearing cartridge in a conventional housing.

[0011] The wells 104, 104' are positioned adjacent to outer sections 110, 110' of the outer race 105, respectively. The outer sections 110, 110' have equal outer diameters that define a clearance with a housing and thereby allow for formation of lubricant films f, f'.

[0012] Fig. 1B shows a cross-sectional view of the prior art cartridge 100 in a prior art housing 160. A pin 162 acts to locate the cartridge 100 axially and azimuthally while allowing freedom in the radial direction. In particular, the pin 162 cooperates with the outer race 105. Axial thrust load along the x-axis causes force to be transmitted from the outer race 105 of the bearing cartridge 100 to the housing 160 via the pin 162. As the pin allows for radial movement, some small amount of clearance exists between the outer diameter of the pin 162 and the inner diameter of the opening 108. Consequently, during operation thrust may cause axial movement of the cartridge with respect to the housing. Such movement can contribute to wear and misalignment.

[0013] The pin 162 also allows for lubricant to flow via a conduit in the pin 162 to a lubricant entrance well 164 adjacent the center section 106 of the cartridge 100. A lubricant exit well 168 exists nearly opposite the entrance well 164 that allows for drainage of lubricant in and about the cartridge 100.

[0014] As shown in Fig. 1B, a clearance exists between an outer diameter of the outer sections 110, 110' and an inner diameter of the housing 160. In this prior art assembly, the clearance defines a single film thickness f. An enlargement of the cross-section shows the single film thickness f as it exists on either side of the well 104. The selection of this clearance (squeeze film thickness) acts to determine the operational characteristics such as rotor radial freedom and damping of rotor imbalance forces.

[0015] Fig. 2 shows a perspective view on an exemplary bearing cartridge 200 that does not include an opening for receiving an axial thrust load pin. The cartridge 200 includes two annular wells 204, 204' positioned on an outer race 205 intermediate a center section 206 and respective ends of the cartridge 200. In this example, the cartridge 200 includes openings 207 and 207' that allow jet lubrication to enter and be directed at the balls of the cartridge 200. Additional openings are optionally included for lubricant flow.

[0016] The wells 204, 204' are positioned adjacent to end sections 210, 210', respectively. The end sections 210, 210' of the outer race 205 have outer diameters that can define clearances with a housing and thereby allow for formation of lubricant films f1, f1', which may be substantially equal.

[0017] Fig. 3 shows a side view of an exemplary cartridge 300 such as the cartridge 200 of Fig. 2. The cartridge 300 includes an outer race 305 having an approximate length L, an approximate axial midpoint L_m and including end sections 310, 310' having outer diameters D_o1, D_o1'. In this example, a drain or lubricant opening 309 is positioned at an axial position at or proximate to the midpoint L_m. The cartridge 300 may include openings such as 207, 207' of the cartridge 200 of Fig. 2. The lubricant opening 309 receives a pin to limit rotation of the outer race 305. The lubricant opening 309 receiving such a rotation limiting pin is still capable of some receiving such a rotation limiting pin is still capable of some radial movement.

[0018] The cartridge 300 includes wells of axial width Δ_w1, Δ_w1' between a center section 306 and end sections 310, 310' with outer diameters D_o1 and D_o1'. The well widths Δ_w1, Δ_w1' may be substantially equal. The outer sections 310, 310' may differ in axial width. For example, the cartridge 300 may include an outer section 310 with outer diameter D_o1 that has an axial width less than the outer section 310' with outer diameter D_o1'.

[0019] The exemplary cartridge 300 includes various parameters that may be used to achieve desired performance characteristics. For example, the axial width and outer diameters of the various sections may be used to define radial clearances/film thicknesses and axial film length(s). In general, judicious selection of thickness, length and number of squeeze films can act to achieve suitable reduction in radial freedom and optimized damping of rotor imbalance forces. Various examples capable of multiple squeeze film thicknesses are described further below with respect to Fig. 8 and Figs. 9A-B.

[0020] Fig. 4 shows a cross-sectional diagram of an exemplary assembly 400 of a turbomachinery device. The assembly 400 includes a bearing cartridge 300 positioned in a housing 440 and located axially with aid of a plate 450. In this example, the plate 450 abuts a surface 446 of the housing 440. A pin 460 received by an opening 444 of the housing 440 aids in locating the cartridge 300 azimuthally with respect to the housing 440. The opening 444 optionally comprises a pin opening having an axis that intersects the central axis (e.g., x-axis) at an angle φ, which is optionally non-orthogonal.

[0021] In this example, the cartridge 300 is located axially with aid of a counterbore 442 of the housing 440 and the plate 450. In general, the plate 450 and the counterbore 442 define an axial distance that is greater than the axial length of the outer race of the bearing cartridge 300. Proper operation of the assembly 400 requires some amount of radial movement; consequently, the axially locating mechanism allows the bearing cartridge to move radially. Further, a clearance may be defined by the difference between the axial distance between a surface of the plate 450 and a surface of the counterbore 442 and the axial length of the outer race of the bearing cartridge 300. Adjustment to such a clearance may be possible via a fixation mechanism of the plate 450 (see, e.g., bolt 452) and/or other features (e.g., gaskets, spacers, etc.).

[0022] Various features of the exemplary assembly 400 also act to directly distribute axial thrust loads to more than one component. For example, the plate 450 can receive thrust loads and the counterbore 442 of the housing 440 can receive axial thrust loads from the bearing cartridge 300. In comparison, the conventional assembly of Fig. 1B transmits axial thrust loads directly and solely to the pin 162. In addition, the exemplary assembly 400 can distribute axial thrust loads over greater surface area when compared to the pin 162 of the conventional assembly of Fig. 1B.

[0023] As already mentioned, the housing 440 includes an opening 444 that receives the pin 460 to aid in azimuthal location of the outer race of the bearing cartridge 300. Such a pin may be referred to as an anti-rotation pin or an azimuthal locating pin because it acts to locate azimuthally and limit rotation of an outer race of a bearing cartridge with respect to a housing. In this example, a lubricant drain opening 448 of the housing 440 allows for insertion of the pin 460 in the opening 444. In this manner, the lubricant drain opening 448 allows drainage of lubricant and insertion and/or adjustment of an anti-rotation pin. While a straight line shows access to the opening 444, access is optionally indirect (e.g., not along a straight line).

[0024] Fig. 5 shows a cross-sectional top view of an exemplary housing 440 and a plate 450. The exemplary housing 440 includes a proximate recessed surface 446 and a distal counterbore 442. The proximate recessed surface 446 is optionally associated with a compressor side of a turbomachinery device and the distal counterbore 442 is optionally associated with a turbine side of a turbomachinery device. Of course, other arrangements are possible.

[0025] The exemplary housing 440 includes an opening 444 set an angle to a central longitudinal housing axis (e.g., x-axis) that allows for insertion of a pin. Such a pin acts to azimuthally locate an outer race of a bearing cartridge in the exemplary housing 440.

[0026] The exemplary housing 440 includes an attachment mechanism for the plate 450. In this example, threaded holes 445, 445' are providing that open along the surface 446. The holes 445, 445' receive bolts 452, 452', respectively. Washers 453, 453' are also shown in this example. Other attachment mechanisms may be used for attaching a plate to a housing. Further, while a substantially circular shaped plate is shown, other shapes are possible and may include one or more surfaces and/or one or more components that act to limit movement of an outer race of a bearing cartridge in the cylindrical bore of a housing in conjunction with a counterbore. An exemplary housing optionally includes an attachment mechanism or mechanisms for one or more limiting components that extend radially inward to a minimum radius less than the inner radius of a cylindrical bore wherein at least some of the components can act to limit axial movement of a bearing cartridge in the cylindrical bore.

[0027] Fig. 6 shows a front view of an exemplary assembly 600 that includes an exemplary housing 440 and an exemplary plate 450. In this example, the plate 450 fits in a recess of the housing 440. The plate 450 acts to define an axial distance along with a counterbore of the housing (not shown in Fig. 6, see, e.g., Fig. 5). In conjunction with an axial length of an outer race of a bearing cartridge, the axial distance acts to define a clearance or clearances between the outer race and the plate 450 and/or the counterbore of the housing 440. The exemplary plate 450 includes four openings 454, 454', 454", 454"' for use in securing the plate 450 to the housing 440. A bolt 452 or other device passes through the opening 454"' to secure the plate 450 to the housing 440. In this example, a washer 453 cooperates with the bolt 452 to secure the plate 450.

[0028] The plate 450 includes an opening 456 that has an inner diameter less than the inner diameter of a substantially cylindrical bore of the housing 440. In this example, the opening 456 is substantially coaxial with the cylindrical bore of the housing 440. A counterbore 442 of the housing 440 has an inner diameter less than the inner diameter of the cylindrical bore of the housing 440. In this example, the counterbore 442 has an arc length less than 360 degrees. Exemplary counterbores may include one or more arc segments, protrusions, etc., that extend inwardly toward a longitudinal or center axis of the cylindrical bore to thereby limit movement of an outer race of a bearing cartridge in the cylindrical bore.

[0029] Fig. 7 shows an exemplary assembly 700 that includes an exemplary plate 750. In this example, the plate 750 is a compressor backplate that fits into the recessed region of a housing 440, for example, at a surface 446. In this example, an attachment mechanism includes use of bolts 752, 752' to secure the plate 750 to the housing 440. The plate 750 extends radially inward past the surface 446 where it further extends past at least a portion of an outer race 305 of a bearing cartridge. The plate 750 includes an opening that has an inner dimension (e.g., a diameter, etc.) that is less than the outer diameter of the outer race 305. While an exemplary plate may include a substantially circular opening with a diameter less than that of an outer race of a bearing cartridge, various exemplary plates may include other shapes, protrusions, etc., that extend inwardly past an inner diameter of a substantially cylindrical bore of a housing to thereby limit axial movement of an outer race of a bearing cartridge. For example, an exemplary plate optionally includes one or more protrusions that extend radially inward toward a central axis to limit movement of an outer race of a bearing cartridge. While not shown in Fig. 7, the housing 440 optionally includes a counterbore to limit movement of the outer race 305, for example, where the plate 750 is positioned at a proximate end of a substantially cylindrical bore of a housing and the counterbore is positioned at distal end of the substantially cylindrical bore of the housing (see, e.g., the counterbore 442 of Fig. 5). Further, the housing 440 of Fig. 7 includes an opening such as the opening 444 of Fig. 5 (e.g., a pin opening, etc.). While such an opening is sometimes referred to herein as a "pin" opening, the term pin may optionally refer to various mechanisms such as screws, bolts, etc., that act to limit rotation of an outer race of a bearing cartridge.

[0030] Fig. 8 shows a cross-sectional diagram of an exemplary bearing cartridge 800 that allows for multiple films of optionally different thicknesses. The cartridge 800 includes a center section 806, intermediate sections 810, 810' and outer sections 812, 812'. The bearing also includes lubricant passages 807, 807' and 809.

[0031] An enlargement shows various wells (e.g., wells, grind reliefs, etc.) and/or transitions from a first outer diameter to a second outer diameter. A wall 866 of a housing or journal having an inner diameter acts to define clearances and film thicknesses f1, f2. In a first scenario 801, wells have curvilinear cross-section; in a second scenario 802, wells have substantially polygonal cross-section; and in a third scenario 803, a step in outer diameter exists between a thick film region f1 and a thinner film region f2. The scenarios 801, 802, 803 are exemplary as others may be used to create clearances that form multiple film thicknesses.

[0032] A housing or journal may act to define clearances that form multiple film thicknesses between the housing and one or more outer diameters of a bearing cartridge. For example, an exemplary housing may include two or more inner diameters that act to define more than one annular clearance with a bearing cartridge and a counterbore to help axially locate the bearing cartridge and/or an opening for receiving a pin to help azimuthally locate an outer race of the bearing cartridge.

[0033] Fig. 9A shows a cross-sectional, side view of an exemplary housing 940 and Fig. 9B shows a cross-sectional top view of the exemplary bearing housing 940. The exemplary housing 940 can house a bearing cartridge and act to define clearances between an outer surface of the bearing cartridge and an inner wall of the housing 940 wherein the clearances act to form various films that can be aimed at reduction of unwanted excessive radial clearance and/or optimized damping of rotor imbalance forces.

[0034] The exemplary housing 940 includes a counterbore 942, an opening 944 and a surface 946 substantially perpendicular to a central axis (e.g., x-axis). The opening 944 optionally comprises a pin opening having an axis that intersects the central axis at an angle φ, which is optionally non-orthogonal. The surface 946 and the counterbore 942 may define a distance that in combination with a bearing cartridge acts to define an axial clearance. A plate (see, e.g., the plate 450 of Fig. 6) cooperates with the surface 946 to define a proximate end of a bearing cartridge chamber while the counterbore 942 defines a distal end of the bearing cartridge chamber.

[0035] The bearing cartridge chamber includes an inner surface 966 that has a first inner diameter and an inner surface 967 that has a second inner diameter wherein the first inner diameter exceeds the second inner diameter. A bearing cartridge that includes an outer surface having an outer diameter may act to define annular clearances with the first and second inner surfaces 966, 967 when positioned in the housing to form an assembly.

[0036] Various exemplary devices, methods, systems, arrangements, etc., described herein pertain to formation and use of multiple film thicknesses. In various examples, one film has damping characteristics and another film has characteristics that minimize excessive radial freedom and play.

[0037] An exemplary bearing cartridge includes an inner film to outer film ratio of approximately 1:2, i.e., the inner film being approximately twice the thickness of the outer film. For example, an inner film of approximately 0.0030 inch (approx. 0.076 mm) and an outer film of approximately 0.0015 inch (approx. 0.0038 mm) wherein the inner film acts to dampen vibrations and the outer film acts to limit rotor radial play. Such an exemplary bearing cartridge may be suitable for use in a commercially available GARRETT® GTA47-55R turbomachinery device (Torrance, California).

[0038] In general, a sufficiently thick film can act to reduce noise and vibration and loading through the system; whereas a thinner film can reduce slop or play in the system (e.g., rotor play, etc.), A thinner film may also allow for reduction in wheel to housing clearances in a turbocharger system, which can act to reduce undesirable secondary aerodynamic flows that would cause reduced compressor and turbine stage thermodynamic efficiencies.

[0039] Various examples include one or more thinner clearance regions proximate to an outer end(s) of a bearing cartridge. A pair of thinner clearance regions proximate to outer ends of a bearing cartridge may limit pivot when compared to a thinner clearance region(s) positioned proximate to or at a center section.

[0040] Although some exemplary methods, devices, systems arrangements, etc., have been illustrated in the accompanying Drawings and described in the foregoing Detailed Description, it will be understood that the exemplary embodiments disclosed are not limiting, but are capable of numerous rearrangements, modifications and substitutions without departing from the invention as defined by the following claims.

Claims

1. A method of limiting movement of an outer race (205, 305) of a bearing cartridge (100, 200, 300, 800) with respect to a housing (160, 440, 940) comprising:

positioning the bearing cartridge (100, 200, 300, 800) in a substantially cylindrical bore having a longitudinal axis (x), an inner diameter exceeding an outer diameter (D_o1, D_o1') of the outer race (205, 305), a proximate end and a distal end;

limiting axial movement of the outer race (205, 305) at the distal end of the cylindrical bore with a counterbore (442, 942) substantially coaxial to the cylindrical bore and having an inner diameter less than the outer diameter (D_o1, D_o1') of the outer race (205, 305);

limiting axial movement of the outer race (205, 305) at the proximate end of the cylindrical bore with a plate (450, 750) positioned substantially orthogonal to the longitudinal axis (x); and

limiting rotation of the outer race (205, 305) with a pin (460) positioned in a pin opening (444, 944) of the housing (160, 440, 940) accessible via a lubricant drain (448).

2. The method of claim 1 wherein the pin axis substantially intersects the longitudinal axis (x) of the cylindrical bore at a non-orthogonal angle (cup).

3. The method of claim 1 wherein the outer race comprises a drain opening (309, 809) to receive the pin (460).

4. The method of claim 1 further comprising providing lubricant and forming lubricant squeeze films (f, f, f₁, f₁', f₂) in clearances between the outer race (205, 305) and the substantially cylindrical bore of the housing.

5. The method of claim 4 wherein the lubricant squeeze films formed comprise multiple squeeze film thicknesses (f₁, f₂).

6. The method of claim 5 further comprising:

forming a first thick lubricant squeeze film (f₁) in an annular clearance between the outer race (205, 305) and the substantially cylindrical bore of the housing and damping bearing vibrations using the first lubricant squeeze film (f₁); and

forming a second thinner lubricant squeeze film (f₂)) in an annular clearance between the outer race (205, 305) and the substantially cylindrical bore of the housing and limiting radial freedom of the bearing using the second lubricant squeeze film (f₂).

7. The method of claim 6 wherein the thickness of the first lubricant squeeze film (f₁) is thicker than the thickness of the second lubricant squeeze film (f₂) by a factor of approximately 2.

8. The method of claim 6 wherein the second thinner lubricant squeeze film (f₂) is formed proximate to an outer end(s) of a bearing cartridge (800).

9. The method of claim 6 further comprising forming a pair of thinner clearance regions with second lubricant squeeze films (f₂) for limiting radial freedom of the bearing in the substantially cylindrical bore using the second lubricant squeeze films (f₂) in the pair of thinner clearance regions.

Ansprüche

1. Verfahren zum Begrenzen der Bewegung einer äußeren Laufbahn (205, 305) einer Lagerpatrone (100, 200, 300, 800) in Bezug auf ein Gehäuse (160, 440, 940), das Folgendes umfasst:

Positionieren der Lagerpatrone (100, 200, 300, 800) in einer im Wesentlichen zylindrischen Bohrung, die eine Längsachse (x), einen Innendurchmesser, der einen Außendurchmesser (D_o1, D_o1') der äußeren Laufbahn (205, 305) übersteigt, ein proximales Ende und ein distales Ende besitzt;

Begrenzen einer axialen Bewegung der äußeren Laufbahn (205, 305) am distalen Ende der zylindrischen Bohrung mit einer Gegenbohrung (442, 942), die zu der zylindrischen Bohrung im Wesentlichen koaxial ist und einen Innendurchmesser besitzt, der kleiner als der Außendurchmesser (D_o1, D_o1') der äußeren Laufbahn (205, 305) ist;

Begrenzen einer axialen Bewegung der äußeren Laufbahn (205, 305) am proximalen Ende der zylindrischen Bohrung mit einer Platte (450, 750), die im Wesentlichen senkrecht zu der Längsachse (x) positioniert ist; und

Begrenzen der Drehung der äußeren Laufbahn (205, 305) mit einem Stift (460), der in einer Stiftöffnung (444, 944) des Gehäuses (160, 440, 940), die durch einen Schmiermittelablauf (448) zugänglich ist, positioniert ist.

2. Verfahren nach Anspruch 1, wobei die Stiftachse die Längsachse (x) der zylindrischen Bohrung unter einem nicht rechten Winkel (ϕ) im Wesentlichen schneidet.

3. Verfahren nach Anspruch 1, wobei die äußere Laufbahn eine Entleerungsöffnung (309, 809) aufweist, um den Stift (460) aufzunehmen.

4. Verfahren nach Anspruch 1, das ferner das Bereitstellen von Schmiermittel und das Bilden von Schmiermittelpressfilmen (f, f', f₁, f₁', f₂) in Zwischenräumen zwischen der äußeren Laufbahn (205, 305) und der im Wesentlichen zylindrischen Bohrung des Gehäuses umfasst.

5. Verfahren nach Anspruch 4, wobei die gebildeten Schmiermittelpressfilme mehrere Pressfilmdicken (f₁, f₂) umfassen.

6. Verfahren nach Anspruch 5, das ferner Folgendes umfasst :

Bilden eines ersten dicken Schmiermittelpressfilms (f₁) in einem ringförmigen Zwischenraum zwischen der äußeren Laufbahn (205, 305) und der im Wesentlichen zylindrischen Bohrung des Gehäuses und Dämpfen von Lagervibrationen unter Verwendung des ersten Schmiermittelfilms (f₁) ; und

Bilden eines zweiten dünneren Schmiermittelpressfilms (f₂) in einem ringförmigen Zwischenraum zwischen der äußeren Laufbahn (205, 305) und der im Wesentlichen zylindrischen Bohrung des Gehäuses und Begrenzen der radialen Freiheit des Lagers unter Verwendung des zweiten Schmiermittelpressfilms (f₂).

7. Verfahren nach Anspruch 6, wobei die Dicke des ersten Schmiermittelpressfilms (f₁) um einen Faktor von ungefähr 2 größer ist als die Dicke des zweiten Schmiermittelpressfilms (f₂).

8. Verfahren nach Anspruch 6, wobei der zweite dünnere Schmiermittelpressfilm (f₂) in der Nähe eines oder mehrerer äußerer Enden der Lagerpatrone (800) gebildet wird.

9. Verfahren nach Anspruch 6, das ferner das Bilden eines Paars dünnerer Zwischenraumbereiche mit zweiten Schmiermittelpressfilmen (f₂) umfasst, um die radiale Freiheit des Lagers in der im Wesentlichen zylindrischen Bohrung unter Verwendung der zweiten Schmiermittelpressfilme (f₂) in dem Paar dünnerer Zwischenraumbereiche zu begrenzen.

Revendications

1. Procédé pour limiter le mouvement d'une bague extérieure (205, 305) d'une cartouche de roulement à billes (100, 200, 300, 800) par rapport à un logement (160, 440, 940), comprenant les étapes suivantes:

- positionner la cartouche de roulement à billes (100, 200, 300, 800) dans un alésage sensiblement cylindrique présentant un axe longitudinal (x), un diamètre intérieur supérieur à un diamètre extérieur (D_o1, D_o1') de la bague extérieure (205, 305), une extrémité proximale et une extrémité distale;

- limiter le mouvement axial de la bague extérieure (205, 305) à l'extrémité distale de l'alésage cylindrique avec un contre-alésage (442, 942) sensiblement coaxial à l'alésage cylindrique et présentant un diamètre intérieur inférieur au diamètre extérieur (D_o1, D_o1') de la bague extérieure (205, 305);

- limiter le mouvement axial de la bague extérieure (205, 305) à l'extrémité proximale de l'alésage cylindrique avec une plaque (450, 750) positionnée sensiblement perpendiculairement à l'axe longitudinal (x); et

- limiter la rotation de la bague extérieure (205, 305) avec une broche (460) positionnée dans une ouverture de broche (444, 944) du logement (160, 440, 940) accessible via un drain pour lubrifiant (448).

2. Procédé selon la revendication 1, dans lequel l'axe de la broche coupe sensiblement l'axe longitudinal (x) de l'alésage cylindrique sous un angle non orthogonal (ϕ).

3. Procédé selon la revendication 1, dans lequel la bague extérieure comporte une ouverture de drain (309, 809) destinée à recevoir la broche (460).

4. Procédé selon la revendication 1, comprenant en outre la fourniture de lubrifiant et la formation de films de lubrifiant écrasés (f, f', f₁, f₁', f₂) dans des espaces entre la bague extérieure (205, 305) et l'alésage sensiblement cylindrique du logement.

5. Procédé selon la revendication 4, dans lequel les films de lubrifiant écrasés formés comprennent plusieurs épaisseurs de films écrasés (f₁, f₂).

6. Procédé selon la revendication 5, comprenant en outre les étapes suivantes:

- former un premier film écrasé épais de lubrifiant (f₁) dans un espace annulaire entre la bague extérieure (205, 305) et l'alésage sensiblement cylindrique et amortir les vibrations du roulement à billes en utilisant le premier film de lubrifiant (f₁) ; et

- former un deuxième film écrasé plus mince de lubrifiant (f₂) dans un espace annulaire entre la bague extérieure (205, 305) et l'alésage sensiblement cylindrique du logement et limiter la liberté radiale du roulement à billes en utilisant le deuxième film écrasé de lubrifiant (f₂).

7. Procédé selon la revendication 6, dans lequel l'épaisseur du premier film écrasé de lubrifiant (f₁) est plus grande que l'épaisseur du deuxième film écrasé de lubrifiant (f₂) d'un facteur d'environ 2.

8. Procédé selon la revendication 6, dans lequel le deuxième film écrasé plus mince de lubrifiant (f₂) est formé à proximité d'une (ou d') extrémité(s) extérieure(s) d'une cartouche de roulement à billes (800).

9. Procédé selon la revendication 6, comprenant en outre la formation d'une paire de régions d'espacement plus minces avec des deuxièmes films écrasés de lubrifiant (f₂) pour limiter la liberté radiale du roulement à billes dans l'alésage sensiblement cylindrique en utilisant les deuxièmes films écrasés de lubrifiant (f₂) dans la paire de régions d'espacement plus minces.

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